# Service difficulty reports: N8887Z, cancelled Sep 11, 2007

A list on [N8887Z, cancelled Sep 11, 2007](https://openairdocs.org/deregistered/N8887Z-2007-09-11.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR C7WA200400051](https://openairdocs.org/sdr/C7WA200400051.md): Stringer · corroded · Sep 22, 2004 · N8887Z · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > STR 27 RT CORRODED STA 620. REMOVED CORROSION IAW SRM 51-10-6 AND INSTALLED STRINGER REPAIR IAW SRM 53-10-4 FIG 1, DETAIL 2.
- [SDR C7WA200400046](https://openairdocs.org/sdr/C7WA200400046.md): Support Angle · corroded · Sep 22, 2004 · N8887Z · Boeing 727225 · Fuselage Miscellaneous Structure
  > SUPPORT ANGLE CORRODED AT STA 1030 TO 1050 BETWEEN STR 29 AND 30 RT. REPAIR ANGLE FABRICATED IAW SAMPLE IAW SRM 51-20-1 AND 51-40-3. MATERIAL USED 7075-T6 X.050 INCH.
- [SDR C7WA200400043](https://openairdocs.org/sdr/C7WA200400043.md): Skin · corroded · Sep 22, 2004 · N8887Z · Boeing 727225 · Fuselage Main, Plate/Skin
  > FUSELAGE LOWER SKIN AT STA 990 STR 28 RT. CORRODED AND TWO RIVETS MISSING. INSTALLED EXTERNAL SKIN REPAIR IAW SRM. 53-30-3 FIG 3. DOUBLER MATERIAL USED, 2024-T3 X.125 INCH X 17 INCHES X 11 INCHES.
- [SDR C7WA200400042](https://openairdocs.org/sdr/C7WA200400042.md): Door Frame · corroded · Sep 22, 2004 · N8887Z · Boeing 727225 · Fuselage Main, Frame
  > ELECTRONIC COMPARTMENT DOOR CUTOUT AFT FRAME CORRODED STA 450 BETWEEN STRINGER 27 RT AND 27 LT. REMOVED AND REPLACED FRAME SECTION. FABRICATED NEW FRAME SECTION IAW SAMPLE. MATER USED 7075-0,.050, HEAT TREATMENT TO 7075-T6 IAW BAC 5602.
- [SDR C7WA200400044](https://openairdocs.org/sdr/C7WA200400044.md): Stringer · corroded · Sep 22, 2004 · N8887Z · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > STRINGER 28 RT CORRODED AT STA 990. REPLACED DAMAGED KEELBEAM SECTION IAW EO NR 1M-727-53-0236 AND DRAWING 65-56441-8.
- [SDR C7WA200400045](https://openairdocs.org/sdr/C7WA200400045.md): Skin · corroded · Sep 22, 2004 · N8887Z · Boeing 727225 · Fuselage Main, Plate/Skin
  > FUSELAGE LOWER SKIN AT STA 720B, STR 28 RT CORRODED. INSTALLED EXTERNAL SKIN REPAIR IAW SRM 53-30-3, FIG 1 DOUBLER MATERIAL USED, 2024-T3 X.160 INCH X 27 INCHES X 28.5 INCHES.
- [SDR C7WA200400050](https://openairdocs.org/sdr/C7WA200400050.md): Stringer · corroded · Sep 22, 2004 · N8887Z · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > STRINGER 29 RT CORRODED AT STA 950A. REMOVED CORROSION IAW SRM 51-10-6 AND INSTALLED REPAIR ON RT FLANGE IAW SB 727-0170.
- [SDR C7WA20040922](https://openairdocs.org/sdr/C7WA20040922.md): Shear Tie · corroded · Sep 22, 2004 · N8887Z · Boeing 727225 · Fuselage Internal Mounting Structure
  > SHEAR TIE CORRODED AT STA 950A BETWEEN STR 28 AND STR 29 RT. REPAIRED SHEAR TIE IAW SRM 53-10-4 FIG 11 MATERIAL USED 7075-T6 X.050 INCH X 6 INCHES X 11 INCHES.
- [SDR C7WA200400048](https://openairdocs.org/sdr/C7WA200400048.md): Shear Tie · corroded · Sep 22, 2004 · N8887Z · Boeing 727225 · Fuselage Main, Structure
  > SHEAR TIE CORRODED AT STA 970 BETWEEN STR 28 AND 29 LT. REPAIRED SHEAR TIE IAW SRM 53-10-4 FIG 11, MATERIAL USED 7075-T6 X.050 INCH X 6 INCHES X 11 INCHES.
- [SDR C7WA200400047](https://openairdocs.org/sdr/C7WA200400047.md): Shear Tie · corroded · Sep 22, 2004 · N8887Z · Boeing 727225 · Fuselage Main, Structure
  > SHEAR TIE CORRODED AT STA 970 BETWEEN STR 28 AND 29 RT. REPAIRED SHEAR TIE IAW SRM 53-10-4 FIG 11. MATERIAL USED 7075-T6 X.050 INCH X 6 INCHES X 11 INCHES.
- [SDR C7WA200400038](https://openairdocs.org/sdr/C7WA200400038.md): Transducer · inoperative · Sep 14, 2004 · N8887Z · Boeing 727225 · Autopilot System
  > AIR RETURN: DURING CLIMBOUT UPPER RUDDER DEFLECTED TO FULL RT YAW DAMPER POSITION THEN BEGAN OSCILLATING LT TO RT CONTINUOUSLY. REMOVED AND REPLACED UPPER YAW DAMPER TRANSDUCER. SYSTEM OPERATIONAL CHECKS NORMAL.
- [SDR C7WA200200040](https://openairdocs.org/sdr/C7WA200200040.md): Pan · cracked · Mar 4, 2003 · N8887Z · Boeing 727225 · Passenger/Crew Doors
  > L1 DOOR VERY HARD TO CLOSE. DURING INSPECTION OF DOOR FOUND CRACKS IN DOOR PAN AROND UPPER AND LOWER TORQUE TUBES. REMOVED AND REPLACED FORWARD ENTRANCE DOOR. (M)
- [SDR C7WA200200039](https://openairdocs.org/sdr/C7WA200200039.md): Duct · loose · Oct 31, 2002 · N8887Z · Boeing 727225 · Pneumatic Distribution System
  > NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED ON TAKEOFF WHILE CLIMBING 200 FEET. EPRS 2.08/2.11. THROTTLES BACKED OFF TO 1.7 EPR LIGHT EXTINGUISHED. TROUBLESHOOTING FOUND DUCT CONNECTION TO NR 3 ENGINE PRECOOLER LOOSE. TIGHTENED, NO FURTHER LEAKS, MM 36-11
- [SDR C7WA200200038](https://openairdocs.org/sdr/C7WA200200038.md): Bracket · misinstalled · Oct 31, 2002 · N8887Z · Boeing 727225 · Landing Gear Door Retract Section
  > UPON GEAR RETRACTION, RED RIGHT GEAR LIGHT AND RED DOORS LIGHT REMAIN ILLUMINATED, AS WELL AS SECOND OFFICERS AMBER RIGHT GEAR DOOR LIGHT, CYCLED GEAR. UPON TROUBLESHOOTING FOUND INBOARD DOOR DRIVE ROD BRACKET INSTALLED BACKWARDS. REPOSITIONED BRACKET AS PER
- [SDR C7WA200200037](https://openairdocs.org/sdr/C7WA200200037.md): Clamp · loose · Oct 30, 2002 · N8887Z · Boeing 727225 · Pneumatic Distribution System
  > NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED ON TAKEOFF, EPRS 2.01/2.03 WHEN THROTTLES BACKED OFF TO 1.7 EPR LIGHT EXTINGUISHED. TIGHTENED LOOSE CLAMP IN STRUT AREA PER MM 75-00 AND 20-80-1. (M)
- [SDR C7WA200200036](https://openairdocs.org/sdr/C7WA200200036.md): Door · out of rig · Oct 30, 2002 · N8887Z · Boeing 727225 · Landing Gear Door Retract Section
  > UPON GEAR RETRACTION RED RIGHT GEAR LIGHT AND RED DOORS LIGHT REMAIN ILLUMINATED. CYCLED GEAR 3 TIMES, NO HELP. AIR TURNBACK. RE-RIGGED RIGHT GEAR DOOR PER MM 32-12-1, PAGE 501-502. GROUND TEST OK. (M)
- [SDR COOSDR00032](https://openairdocs.org/sdr/COOSDR00032.md): Fitting · corroded · Feb 15, 2001 · N8887Z · Boeing 727225 · Main Landing Gear Attach Section
  > INSPECTION REPORTED A CORRODED FORWARD SUPPORT TRUNNION BEARING FITTING ON THE LEFT SIDE OF THE AIRCRAFT.
- [SDR COOSDR000033](https://openairdocs.org/sdr/COOSDR000033.md): Torque Box · fatigued · Feb 15, 2001 · N8887Z · Boeing 727225 · Fuselage Miscellaneous Structure
  > COOPESA REPORTED THE NOSE WHEEL WELL TORQUE BOX LOWER CHORD LBL 19, WL 148 CHORD WITH CORROSION. REPLACED THE SUBJECT CHORD. PROBABLE CAUSE OF CORROSION WAS FATIGUE.

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N8887Z' AND deregistration_id = 'N8887Z-2007-09-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N8887Z-2007-09-11/reports

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